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A Method Of Calculating The Compressive Strength Of Z Stiffened Panels That Develop Local Instability by George L. Gallaher
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1NASA Technical Reports Server (NTRS) 19930082136: A Method Of Calculating The Compressive Strength Of Z-stiffened Panels That Develop Local Instability
By NASA Technical Reports Server (NTRS)
“NASA Technical Reports Server (NTRS) 19930082136: A Method Of Calculating The Compressive Strength Of Z-stiffened Panels That Develop Local Instability” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19930082136: A Method Of Calculating The Compressive Strength Of Z-stiffened Panels That Develop Local Instability
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_19930082136
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The book is available for download in "texts" format, the size of the file-s is: 6.55 Mbs, the file-s for this book were downloaded 88 times, the file-s went public at Sat Mar 12 2016.
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Abbyy GZ - Animated GIF - Archive BitTorrent - DjVuTXT - Djvu XML - Item Tile - Metadata - Scandata - Single Page Processed JP2 ZIP - Text PDF -
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2A Method Of Calculating The Compressive Strength Of Z-stiffened Panels That Develop Local Instability
By Gallaher, George L and Boughan, Rolla
No Abstract Available
“A Method Of Calculating The Compressive Strength Of Z-stiffened Panels That Develop Local Instability” Metadata:
- Title: ➤ A Method Of Calculating The Compressive Strength Of Z-stiffened Panels That Develop Local Instability
- Authors: Gallaher, George LBoughan, Rolla
- Language: English
“A Method Of Calculating The Compressive Strength Of Z-stiffened Panels That Develop Local Instability” Subjects and Themes:
- Subjects: ➤ AIRFOILS - NACA 66(109)-210 (A=1 0,CLI=0 6)- CHAR ,MOMENTS & (A=0 6,CLI=-0 4) - ORDINATES - LOW-DRAG - AIRFOILS - NACA 66-210 - CHAR & MOMENTS - LOW-DRAG - AIRFOILS, CAMBERED - CHARACTERISTICS - WIND TUNNEL TESTS - WIND TUNNEL TESTS - AAL - HIGH-SPEED (3 1/2'X1') - WORK CARRIED ON AT AAL - AIRFOILS - CHARACTERISTICS - EFFECT OF COMPRESSIBILITY - PRESSURE DISTRIBUTION - AIRFOILS - NACA 66(109)-210
Edition Identifiers:
- Internet Archive ID: nasa_techdoc_19930082136
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 2.62 Mbs, the file-s for this book were downloaded 261 times, the file-s went public at Sat May 21 2011.
Available formats:
Abbyy GZ - Animated GIF - Archive BitTorrent - DjVu - DjVuTXT - Djvu XML - Item Tile - Metadata - Scandata - Single Page Processed JP2 ZIP - Text PDF -
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- Whefi.com: Download
- Whefi.com: Review - Coverage
- Internet Archive: Details
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